The proposed technology will provide an accurate and comprehensive analysis tool for coupled AeroPropulsoServoElastic (APSE) simulations of supersonic vehicles especially for the next generation and beyond (N+2) supersonic transport aircraft. The APSE tool will help in the design of supersonic aircraft that are safer, have better ride quality, and easier to fly. It will enable NASA to analyze interaction characteristics of fluid, structural, thermal, propulsive and controls fields of aerospace vehicles. NASA direct applications include supersonic vehicles, hypersonic re-entry vehicles, inflatable aerodynamic decelerators, hypersonic aircraft and spacecraft (X-51), NASA's Orion crew exploration vehicle, the Commercial Orbital Transportation Services (COTS) vehicle, and many others. Ultimately, the framework will lead to improved performance and safety of aerospace vehicles and significantly reduce the dependence on flight tests and wind tunnel testing thereby reducing the time required to certify new NASA, military and commercial aircraft and spacecraft.
Non-NASA potential customers and applications include DoD agencies such as U.S. Air Force, U.S. Navy, DARPA, U.S. Army and Missile Defense agencies and contractors such as Lockheed Martin and Boeing for application involving development of flexible supersonic manned and unmanned air vehicles as well as global strike hypersonic vehicles. Other commercial applications include general multi-disciplinary analysis problems such as heat exchanger vibration, panel flutter of aerospace vehicles, turbo-machinery blade vibrations and many others.
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